Pages that link to "Item:Q1637799"
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The following pages link to A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary (Q1637799):
Displaying 7 items.
- Highly physical penumbra solar radiation pressure modeling with atmospheric effects (Q748292) (← links)
- Canonical modelling of relative spacecraft motion via epicyclic orbital elements (Q816892) (← links)
- Relative motion of satellites exploiting the super-integrability of Kepler's problem (Q968345) (← links)
- A satellite relative motion model including \(J_2\) and \(J_3\) via Vinti's intermediary (Q1637799) (← links)
- Nonlinear analytic solution for perturbed relative motion using differential equinoctial elements (Q2203829) (← links)
- The Lagrange coefficients of Vinti theory (Q2210850) (← links)
- Satellite prediction formulae for Vinti's model (Q5578333) (← links)